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<!--BEGIN SPECIFICATIONS--> F-15 ACTIVE Specifications Primary Function: experimental - Advanced Control Technology for Integrated Vehicles Contractor: McDonnell Douglas Crew: Two Unit Cost: N/A Powerplant Two higher-thrust version Pratt & Whitney F100-PW-229 engines (with newly developed axisymmetric thrust-vectoring engine exhaust nozzles) rated at 29,000 lbs. of thrust each at full power Dimensions Length: 63.7 ft, excluding flight test nose boom Wingspan: 42.8 ft Canard span: 25.6 ft Height: 18.5 ft - F-15 Weights Empty: 35,000 lb TOW: 47,000 lb Performance Speed: Mach 2.0 (speeds limited to Mach 1.2) Ceiling: 60,000 feet Range: N/A Armament N/A <!--END SPECIFICATIONS--> <!--BEGIN ACHIEVEMENTS--> F-15 ACTIVE Achievements The F-15 ACTIVE demonstrated the first supersonic yaw-vectoring flight The F-15 ACTIVE demonstrated the first pitch and yaw thrust vectoring at speeds up to Mach 2 The F-15 ACTIVE was the first two-seat F-15 built by McDonnell Douglas <!--END ACHIEVEMENTS--> <!--BEGIN FEATURES--> <!-- F-15 ACTIVE Features --> <!--END FEATURES--> <!--BEGIN BACKGROUND--> <!-- F-15 ACTIVE Background --> <!--END BACKGROUND-->
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